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EN 1.4416 Stainless Steel vs. 6016 Aluminum

EN 1.4416 stainless steel belongs to the iron alloys classification, while 6016 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is EN 1.4416 stainless steel and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
55 to 80
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 34
11 to 27
Fatigue Strength, MPa 170
68 to 89
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 79
26
Tensile Strength: Ultimate (UTS), MPa 500
200 to 280
Tensile Strength: Yield (Proof), MPa 210
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Maximum Temperature: Mechanical, °C 1100
160
Melting Completion (Liquidus), °C 1450
660
Melting Onset (Solidus), °C 1400
610
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 12
190 to 210
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 1.9
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.5
Density, g/cm3 8.1
2.7
Embodied Carbon, kg CO2/kg material 5.8
8.2
Embodied Energy, MJ/kg 79
150
Embodied Water, L/kg 190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 110
82 to 340
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 17
21 to 29
Strength to Weight: Bending, points 17
29 to 35
Thermal Diffusivity, mm2/s 3.2
77 to 86
Thermal Shock Resistance, points 12
9.1 to 12

Alloy Composition

Aluminum (Al), % 0
96.4 to 98.8
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 19 to 21
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 45.2 to 52.4
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0 to 1.0
0 to 0.2
Molybdenum (Mo), % 4.5 to 5.5
0
Nickel (Ni), % 24 to 26
0
Nitrogen (N), % 0.12 to 0.2
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
1.0 to 1.5
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15